# Boeing 727-27

- Type: Aircraft model (FAA registry)
- Registry code: 138400K
- Manufacturer (registry): BOEING
- Model: 727-27
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 3 · Turbo-jet
- Seats: 134
- Weight class: 20,000 lb and over
- Cruise speed: 435 mph
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-727-27

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

None matched.

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19870530029409I](https://openairdocs.org/incident/19870530029409I), May 30, 1987: Boeing 727100 (N803SC), Bonaire, NA. During back taxi smoke was seen from the left side of plane. Evacuation. Oil mist venting through engine breather.

## Service difficulty reports (7)

As reported by operators and repair stations, by the model named in the report.

- [SDR C1HA200296002](https://openairdocs.org/sdr/C1HA200296002), Jan 6, 2002: BLEED VALVE. MALFUNCTIONED. POWER UP FOR TAKEOFF NR 2 ENGINE COMPRESSOR STALLED POWER WAS AT 1.6 EPR AND SPEED WAS BELOW 40 KTS. NR 2 PRBC WAS CHANGED AND OPS CHECK GOOD AND NR 2 GENERATOR
- [SDR C1HA200296001](https://openairdocs.org/sdr/C1HA200296001), Jan 6, 2002: ENGINE. MALFUNCTIONED. ON RUNWAY ADVANCED THROTTLE TO 1.4 CHECK PARAMETERS GOOD, CONTINUED THROTTLE ADVANCE FORFLEX POWER, LOUD BANG FROM NR 2 ENGINE, ENGINE FAIL LIGHT ILLUMINATED AN
- [SDR 98ZZZX2491](https://openairdocs.org/sdr/98ZZZX2491), Jun 2, 1998: BEAM. CORRODED. DURING C-CHECK, EXFOLIATION CORROSION ON LEFT HORIZONTAL UPPER TRAILING EDGE BEAM BETWEEN STA 99.8 AND STA 136.5.
- [SDR 97FDEA00741](https://openairdocs.org/sdr/97FDEA00741), Oct 14, 1997: STRINGER. CORRODED. WHILE WORKING NR 0696 UPON REMOVAL OF STRINGER FROM BS 610 TO 624, STR 28 LT TO ACCESS KEEL BEAM CORROSION FOUND CORROSION IN BETWEEN SURFACES OF KEEL BEAM AND 
- [SDR 97FDEA00491](https://openairdocs.org/sdr/97FDEA00491), Jul 30, 1997: STRINGER. CORRODED. CORROSION (C53-224-012) ON STR 4 LT, BS 804 TO 870. *S/D* REPAIRED DAMAGED AREA OF STR 4 LT, BS 845 IAW FED-EX SRM 53-10-3.
- [SDR 96FDEA01414](https://openairdocs.org/sdr/96FDEA01414), Aug 27, 1996: ACM. OIL LEAK. SMOKE IN CARGO COMPARTMENT. NOT RECOGNIZABLE ODOR. REQUIRED USE OF OXYGEN MASKS AND EMERGENCY DESCENT. FOUND OLD ACM LEAKING OIL AND BYPASSING INTERNALLY CAUSIN
- [SDR 96FDEA00242](https://openairdocs.org/sdr/96FDEA00242), Feb 1, 1996: SKIN. CORRODED. BS 720 O/B SIDE OF STR 28 RT, FUSELAGE SKIN IS BULGING. CUT OUT DAMAGE AREA 1 INCH BY 2 INCH AND INSTALLED DOUBLER PER SRM 51-0-6.

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